Models having aspect ratios ranging from 2 to 13 were tested at Mach numbers up to 0.92; examination of data is made on basis of reference theoretical values obtained from 2-dimensional incompressible flow theory; on this basis reduction in aspect ratio increased ratio of experimental to calculated flutter speed.


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    Title :

    Experimental investigation of effect of aspect ratio and Mach number on flutter of cantilever wings


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :



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    Tuovila, W J / Baker, John E / Regier, Arthur, A | NTRS | 1954


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    Tuovila, W.J. / Baker, J.E. / Regier, A.A. | Engineering Index Backfile | 1954